IT8448432A0 - SYSTEM AND METHOD FOR INTENSIFYING THE THERMOENERGY CYCLE IN PROPULSION ENGINES BY MEANS OF AIR JET AND RELATED IMPROVED ENGINES - Google Patents
SYSTEM AND METHOD FOR INTENSIFYING THE THERMOENERGY CYCLE IN PROPULSION ENGINES BY MEANS OF AIR JET AND RELATED IMPROVED ENGINESInfo
- Publication number
- IT8448432A0 IT8448432A0 IT8448432A IT4843284A IT8448432A0 IT 8448432 A0 IT8448432 A0 IT 8448432A0 IT 8448432 A IT8448432 A IT 8448432A IT 4843284 A IT4843284 A IT 4843284A IT 8448432 A0 IT8448432 A0 IT 8448432A0
- Authority
- IT
- Italy
- Prior art keywords
- engines
- thermoenergy
- intensifying
- cycle
- air jet
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/08—Heating, heat-insulating or cooling means
- F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/12—Cooling of plants
- F02C7/16—Cooling of plants characterised by cooling medium
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/16—Composite ram-jet/turbo-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
- F23R3/34—Feeding into different combustion zones
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Means For Warming Up And Starting Carburetors (AREA)
- Control Of Turbines (AREA)
- Percussion Or Vibration Massage (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US50565883A | 1983-06-20 | 1983-06-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
IT8448432A0 true IT8448432A0 (en) | 1984-06-20 |
IT1177817B IT1177817B (en) | 1987-08-26 |
Family
ID=24011258
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
IT48432/84A IT1177817B (en) | 1983-06-20 | 1984-06-20 | SYSTEM AND METHOD FOR INTENSIFYING THE THERMO-ENERGY CYCLE IN PROPULSION ENGINES BY AIR JET AND RELATED IMPROVED ENGINES |
Country Status (9)
Country | Link |
---|---|
EP (1) | EP0146624B1 (en) |
JP (1) | JPS60501616A (en) |
AU (1) | AU3210384A (en) |
BR (1) | BR8406943A (en) |
CA (1) | CA1235583A (en) |
DE (1) | DE3477229D1 (en) |
DK (1) | DK77385D0 (en) |
IT (1) | IT1177817B (en) |
WO (1) | WO1985000199A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4858428A (en) * | 1986-04-24 | 1989-08-22 | Paul Marius A | Advanced integrated propulsion system with total optimized cycle for gas turbines |
US4916896A (en) * | 1988-11-02 | 1990-04-17 | Paul Marius A | Multiple propulsion with quatro vectorial direction system |
FR2670869B1 (en) * | 1990-12-19 | 1994-10-21 | Snecma | COMBUSTION CHAMBER COMPRISING TWO SUCCESSIVE SPEAKERS. |
JP2988109B2 (en) * | 1991-03-20 | 1999-12-06 | 株式会社日立製作所 | Rotor shaft for rotating electric machine and rotating electric machine using the same |
GB9418949D0 (en) * | 1994-09-20 | 1994-11-09 | Helliwell Brian J | 90% thermal efficient gas turbine engine |
DE19902437C5 (en) * | 1999-01-22 | 2017-01-12 | General Electric Technology Gmbh | Method and device for rapid startup and for rapid increase in output of a gas turbine plant |
EP2622192A2 (en) * | 2010-09-30 | 2013-08-07 | General Electric Company | Aircraft engine systems and methods for operating same |
WO2012173651A1 (en) * | 2011-06-17 | 2012-12-20 | General Electric Company | Aircraft engine fuel system and method of operating the same |
US9709069B2 (en) | 2013-10-22 | 2017-07-18 | Dayspring Church Of God Apostolic | Hybrid drive engine |
JP7250304B2 (en) * | 2018-09-26 | 2023-04-03 | 国立大学法人室蘭工業大学 | Propellant for gas generator for turbine drive and method for producing the same |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2360130A (en) * | 1941-03-26 | 1944-10-10 | Armstrong Siddeley Motors Ltd | High-speed propulsion plant |
US2416389A (en) * | 1942-06-17 | 1947-02-25 | Armstrong Siddeley Motors Ltd | Torque balancing of jet propulsion turbine plant |
FR924012A (en) * | 1946-02-18 | 1947-07-24 | Const Aeronautiques Du Ct Soc | Further development of combustion turbines |
US2647368A (en) * | 1949-05-09 | 1953-08-04 | Hermann Oestrich | Method and apparatus for internally cooling gas turbine blades with air, fuel, and water |
DE846341C (en) * | 1950-06-20 | 1952-08-11 | Gustav Fillon | Blading with internal cooling for gas turbines with combustion within the blade channels |
CH308992A (en) * | 1951-05-16 | 1955-08-15 | Power Jets Res & Dev Ltd | Gas turbine plant. |
US2970807A (en) * | 1957-05-28 | 1961-02-07 | Messerschmitt Ag | Rotor blades for gas turbines |
US3747339A (en) * | 1961-11-13 | 1973-07-24 | Texaco Inc | Reaction propulsion engine and method of operation |
DE1231959B (en) * | 1963-06-28 | 1967-01-05 | M A N Turbo G M B H | As a twin-flow engine in single-shaft design, lift jet engine for aircraft |
GB1039677A (en) * | 1963-07-10 | 1966-08-17 | Rolls Royce | Combustion chamber for a gas turbine engine |
US3740949A (en) * | 1963-11-20 | 1973-06-26 | Texaco Inc | Fuel cooled ram air reaction propulsion engine |
DE1261357B (en) * | 1965-12-14 | 1968-02-15 | Dornier Gmbh | Gas turbine engine |
US3486340A (en) * | 1967-05-05 | 1969-12-30 | Garrett Corp | Gas turbine powerplant with means for cooling compressed air |
US3600890A (en) * | 1968-11-29 | 1971-08-24 | United Aircraft Corp | Turbine cooling construction |
CH573571A5 (en) * | 1974-01-11 | 1976-03-15 | Sulzer Ag | |
US4054030A (en) * | 1976-04-29 | 1977-10-18 | General Motors Corporation | Variable cycle gas turbine engine |
US4118145A (en) * | 1977-03-02 | 1978-10-03 | Westinghouse Electric Corp. | Water-cooled turbine blade |
US4190398A (en) * | 1977-06-03 | 1980-02-26 | General Electric Company | Gas turbine engine and means for cooling same |
US4242045A (en) * | 1979-06-01 | 1980-12-30 | General Electric Company | Trap seal for open circuit liquid cooled turbines |
-
1984
- 1984-06-19 CA CA000456928A patent/CA1235583A/en not_active Expired
- 1984-06-20 BR BR8406943A patent/BR8406943A/en unknown
- 1984-06-20 DE DE8484902846T patent/DE3477229D1/en not_active Expired
- 1984-06-20 JP JP59502830A patent/JPS60501616A/en active Pending
- 1984-06-20 AU AU32103/84A patent/AU3210384A/en not_active Abandoned
- 1984-06-20 WO PCT/US1984/000935 patent/WO1985000199A1/en active IP Right Grant
- 1984-06-20 IT IT48432/84A patent/IT1177817B/en active
- 1984-06-20 EP EP84902846A patent/EP0146624B1/en not_active Expired
-
1985
- 1985-02-20 DK DK77385A patent/DK77385D0/en unknown
Also Published As
Publication number | Publication date |
---|---|
DK77385A (en) | 1985-02-20 |
EP0146624B1 (en) | 1989-03-15 |
DK77385D0 (en) | 1985-02-20 |
JPS60501616A (en) | 1985-09-26 |
WO1985000199A1 (en) | 1985-01-17 |
DE3477229D1 (en) | 1989-04-20 |
CA1235583A (en) | 1988-04-26 |
BR8406943A (en) | 1985-06-04 |
EP0146624A4 (en) | 1986-03-18 |
EP0146624A1 (en) | 1985-07-03 |
IT1177817B (en) | 1987-08-26 |
AU3210384A (en) | 1985-01-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19921230 |